de Havilland Canada DHC-2 Beaver

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DHC-2 Beaver
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A de Havilland Canada DHC-2 Beaver Mk1 on floats
Role STOL utility transport
National origin Canada
Manufacturer de Havilland Canada
First flight August 16, 1947
Introduction 1948
Status Production completed
Primary users regional and remote air carriers
United States Army
Civil Air Patrol
Produced 1947–1967
Number built 1,657
Developed into DHC-3 Otter

The de Havilland Canada DHC-2 Beaver is a single-engined, high-wing, propeller-driven, STOL aircraft developed by de Havilland Canada, primarily known as a bush plane. It is used for cargo and passenger hauling, aerial application (crop dusting and aerial topdressing), and has been widely adopted by armed forces as a utility aircraft. The United States Army purchased several hundred; nine DHC-2s are still in service with the U.S. Air Force Auxiliary (Civil Air Patrol) for search and rescue. A Royal New Zealand Air Force Beaver supported Sir Edmund Hillary's expedition to the South Pole. Over 1,600 Beavers were produced until 1967 when the original line shut down.[1]

Due to its success, the Royal Canadian Mint commemorated the Beaver on a special edition Canadian quarter in November 1999.

Design and development

File:De Havilland Canada DHC-2 Beaver (N130WA).jpg
A Beaver, operated by Freebird Wilderness Tours, at Airport Niederrhein in Germany
File:De Havilland Canada DHC-2 Beaver N72355 Kenmore 2 crop.jpg
A de Havilland Canada DHC-2 Beaver operated by Kenmore Air on floats.
File:Instrument panel of a deHavilland Canada DHC-2 Beaver.JPG
Instrument panel of a DHC-2 -- note the single pilot's yoke, that can be handed over to the co-pilot, in flight.
Ontario Ministry of Natural Resources deHavilland DHC-2 Mk 3 Turbo Beavers on amphib floats in Dryden, Ontario in 1995
File:DHC-2T Beaver C6-BIQ Bartow 30.03.11R 1647 edited-2.jpg
Wipaire Boss Beaver conversion with PT6 turbo engine retaining original fin shape and fitted with floats at Bartow Municipal Airport, Florida in 2011

After the war, de Havilland Canada management turned to the civilian market for work, aware that military contracts were unlikely to guarantee business. The company had recently hired Punch Dickins, a famous bush pilot, as Director of Sales who began an extensive program of collecting requests from other pilots, to understand what they needed in a new aircraft. Almost without variation, the pilots asked for tremendous extra power and STOL performance, in a design that could be easily fitted with wheels, skis or floats. When de Havilland engineers noted that this would result in poor cruise performance, one pilot replied "You only have to be faster than a dog sled". Other suggestions were seemingly mundane but important in the bush plane world; full-sized doors were installed on both sides of the aircraft so it could be easily loaded no matter which side of a dock it tied up on. The doors were also made wide enough to allow for a 45 Imperial gallon drum to be rolled up into the aircraft.

On September 17, 1946, de Havilland officially put together a design team consisting of Fred Buller, Dick Hiscocks, Jim Houston and W. Jakimiuk, led by Phil Garratt. The new aircraft was designed to be all-metal (unlike older designs like the famous Noorduyn Norseman), using "steel from the engine to the firewall, heavy aluminum truss frames with panels and doors throughout the front seat area, lighter trusses toward the rear and all monocoque construction aft". At the time de Havilland Canada was still a British-owned company and there were plans to fit the evolving design with a British engine. This limited power, so the wing area was greatly increased in order to maintain STOL performance. When Pratt & Whitney Canada offered to supply war-surplus 450 hp (340 kW) Wasp Jr engines at a low price, the aircraft ended up with extra power as well as the original long wing. The result was unbeatable STOL performance for an aircraft of its size.

After much testing and with adjustments and improvements, the innovative airplane was ready for the sales circuit. Since de Havilland Canada aircraft were all named after animals, it was decided that the new bush plane was much like the hard-working beaver. The first flight of the DHC-2 Beaver was in Downsview, Ontario by Second World War flying ace Russell Bannock on August 16, 1947. The first production aircraft was delivered to the Ontario Department of Lands and Forests, a design partner, in April 1948.

Initial sales were slow, perhaps two or three a month but as the plane was demonstrated sales started to improve. A key event in the Beaver's history occurred the next year, when the US Army started looking for a new utility aircraft to replace their Cessnas. The competition quickly boiled down to the Beaver and the Cessna 195 but the Beaver outperformed the 195 and with the outbreak of the Korean War, led to orders for hundreds of aircraft. Soon orders increased from around the world. When production finally ceased in 1967, 1,657 DHC-2 Beavers had been built.

The Beaver was designed for flight in rugged and remote areas of the world. Its short takeoff and landing capability made it ideal for areas normally only accessible by canoe or foot. Because it often flies to remote locations, often in cold climates, its oil reservoir filler is located in the cockpit and oil can be filled in flight. A series of upgrades to the basic design were incorporated. One major customer introduced the use of flat steps replacing the earlier tubes, a feature that is now almost universal. In 1987, the Canadian Engineering Centennial Board named the DHC-2 one of the top ten Canadian engineering achievements of the 20th century.[2]

Recent developments

A Beaver on floats
DHC-2 MK. III Turbo Beaver

At one point in its production, plans to license and build the type in New Zealand were proposed. The remaining tooling was purchased by Viking Air of Victoria, Canada, which manufactures replacement parts for most of the early de Havilland line. On 24 February 2006, Viking purchased the type certificates from Bombardier Aerospace for all the original de Havilland designs.[3] The ownership of the certificates gives Viking the exclusive right to manufacture new Beavers. Viking now sells a remanufactured and rebuilt DHC-2T Turbo Beaver upgraded with a Pratt & Whitney Canada PT6A-34 680 hp (507 kW) turboprop engine. With a maximum gross takeoff weight increased to 6,000 lb (2,700 kg) it can carry 2,450 lb (1,110 kg) of freight.[4] However, Viking Turbo Beavers are only rebuilt from existing air frames, and are not new-builds, unlike Viking's own DHC-6 Series 400 Twin Otter, which is manufactured from a completely new airframe.

Operational history

File:RNZAFTransantarcticDHCBeaver.jpg
RNZAF Beaver that supported the Commonwealth Trans-Antarctic Expedition.
File:600hpDH2.jpg
600 hp (447 kW) PZL engine modification

Despite the fact that production ceased in 1967, hundreds of Beavers are still flying—many of them heavily modified to adapt to changes in technology and needs. Kenmore Air of Kenmore, Washington provides Beaver and Otter airframes with zero-hour fatigue-life ratings, and owns dozens of supplemental type certificates (STCs) for aircraft modifications. These modifications are so well known and desirable in the aviation community, rebuilt Beavers are often called "Kenmore Beavers" or listed as having "Kenmore mods" installed.[5]

The original Wasp Jr radial engine of the Beaver is long out of production, so repair parts are getting harder to find. Some aircraft conversion stations have addressed this problem by replacing the piston engine with a turboprop engine such as the PT6. The added power and lighter installed weight, together with greater availability of kerosene fuel instead of high-octane aviation gasoline, make this a desirable modification, but at a high financial cost.

The Beaver was deployed by the British Army Air Corps during the Troubles at least until 1979 for photo-reconnaissance missions. One of them was hit seven times by machine gun fire in South County Armagh, near the border with the Republic of Ireland in November 1979, while taking valuable photos of an IRA checkpoint. The border crossing where the action took place was known by the British Army as "Beaver Junction" since then.[6]

Operators of significant numbers of piston-Beavers in early 2008 include Air Saguenay and Harbour Air in Canada and Kenmore Air in the USA.[7]

Harrison Ford owns a DHC-2 Beaver and has called it his favourite among his entire fleet of private aircraft.[8]

The United States military continues to operate two DHC-2s at the United States Naval Test Pilot School, where they are used to instruct students in the evaluation of lateral-directional flying qualities and to tow gliders.

The DHC-2 Beaver is sometimes used by skydiving operators due to its good climb rate. When fitted with a roller door that can be opened in flight, it can quickly ferry eight skydivers to 13,000 ft (4,000 m).

Stolairus Aviation of Kelowna, British Columbia has developed several modifications for the DHC-2 including a STOL Kit which modifies the wing with a contoured leading edge, flap-gap seals, wing fences and drooped wingtips for increased performance. Stolairus has also developed a Wing Angle Kit which changes the incidence of the wing.[9]

Advanced Wing Technologies of Vancouver, British Columbia has developed and certified a new wing for the DHC-2. The FAA Supplemental Type Certificate also raises the aircraft's gross weight to 6,000 lb (2,700 kg).[10] So far, at least two Beavers have been so modified.[11][12]

Variants

Beaver I
Single-engined STOL utility transport aircraft.
Beaver AL Mk 1
STOL utility transport aircraft for the British Army.
C-127
original designation for DHC-2 aircraft used by the U.S. military, redesignated L-20.[13]
YL-20
Test and evaluation aircraft for the US military.
L-20A Beaver
STOL utility transport aircraft for the U.S. Army, later redesignated U-6A in 1962, 968 built.
L-20B Beaver
Basically similar to the L-20A, but with minor equipment changes. Six were sold to the US Army. Later redesignated U-6B in 1962.
U-6A
US Army L-20A aircraft re-designated
U-6B
US Army L-20B aircraft re-designated
Beaver II
One aircraft was fitted with an Alvis Leonides radial piston engine.[14]
Wipaire Super Beaver
Conversion of surplus US Army and USAF L-20 Beavers.[citation needed]
Wipaire Boss Turbo-Beaver
Turbo conversion fitted with PT-6 but retaining the original lower curved fin shape
Turbo-Beaver III
Powered by a 431 kW (578 ehp) Pratt & Whitney PT6A-6 or -20 turboprop engine.
Airtech Canada DHC-2/PZL-3S
After-market conversion by Airtech Canada in the 1980s, using current-production PZL-3S radial engines of 600 hp (450 kW)
Volpar Model 4000
Was a 1970s conversion by Volpar, first flown in April 1972 with a modified nose fitted with an AiResearch TPE331-2U-203 turboprop with a three-bladed propeller. Other changes included a new fin and rudder.[15]
Viking DHC-2T Turbo Beaver
Remanufactured Beavers by Viking Air, upgraded with a Pratt & Whitney Canada PT6A-34 680 hp (507 kW) turboprop engine.[16]

Operators

Civil

The DHC-2 is popular with air charter companies, police forces and small air taxi operators as well as private individuals and companies. Both the Royal Canadian Mounted Police and Finnish Border Guard operate the aircraft.

Military operators

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File:De Havilland Beaver DA-SC-99-04701.jpg
U.S. Army example
File:U-6A Beaver.jpg
U-6A Beaver at the National Museum of the United States Airforce
File:U6-Beaver.png
U-6A Beaver aircraft on display
 Argentina
 Australia
 Austria
 Burma
 Cambodia
 Chile
 Taiwan
 Colombia
 Cuba
 Dominican Republic
 Finland
 France
 Ghana
 Greece
 Haiti
 Indonesia
 Iran
 Kenya
 Laos
 Netherlands
 New Zealand
 Oman
 Panama
 Paraguay
 Peru
 Philippines
Federation of South Arabia Federation of South Arabia
  • Federation of South Arabian Air Force
 South Vietnam
 South Yemen
  • South Yemen Air Force
 Thailand
 Turkey
 Uganda
 United Kingdom
 United States
 Yugoslavia
 Zambia

Accidents and incidents

There have been 183 incidents involving the DHC-2 and 404 deaths.[20]

Aircraft on display

Specifications (DHC-2)

Orthographically projected diagram of the de Havilland Canada DHC-2 Beaver.

Data from Donald 1997, p. 328.

General characteristics

  • Crew: 1
  • Capacity: 6 passengers, 2,100 lb (953 kg) useful load
  • Length: 30 ft 3 in (9.22 m)
  • Wingspan: 48 ft 0 in (14.63 m)
  • Height: 9 ft 0 in (2.74 m)
  • Wing area: 250 ft2 (23.2 m2)
  • Empty weight: 3,000 lb (1,361 kg)
  • Gross weight: 5,100 lb (2,313 kg)
  • Powerplant: 1 × Pratt & Whitney R-985 Wasp Jr. radial engine, 450 hp (336 kW) each

Performance

  • Maximum speed: 158 mph (255 km/h)
  • Cruise speed: 143 mph (230 km/h)
  • Range: 455 miles (732 km)
  • Service ceiling: 18,000 ft (5,486 m)
  • Rate of climb: 1,020 ft/min (5.2 m/s)

See also

Related development
Aircraft of comparable role, configuration and era

References

Notes
  1. ↑ 1.0 1.1 "de Havilland Canada DHC-2 Beaver." Canada Aviation and Space Museum. Retrieved: November 20, 2009.
  2. ↑ Cooper, Russ. "Winged Workhorse." Canadian Geographic magazine, July/August 2007, p. 26.
  3. ↑ "Viking acquires DeHavilland type certificates." Viking Press Release, February 24, 2006.
  4. ↑ "DHC-2T Turbo Beaver: The Legend Continues." vikingair.com. Retrieved: November 20, 2009.
  5. ↑ "Beaver Rebuild Program." Kenmore Air, May 21, 2007. Retrieved: November 20, 2009.
  6. ↑ Harnden 2000, pp. 172–173.
  7. ↑ Pither 2008, pp. 57, 79, 382.
  8. ↑ "Harrison Ford Discusses Piloting His Beaver Into The Bush." Huffington Post, May 2008. Retrieved: November 20, 2009.
  9. ↑ "DHC-2 Beaver." Stolairus Retrieved: February 2, 2012.
  10. ↑ "FAA STC SA00857NY Installation of a new Advanced Wing Technologies (AWT) wing and increase in gross weight to 6000 pounds." FAA. Retrieved: July 3, 2011.
  11. ↑ "Beaver Tails c/n 31." dhc-2.com. Retrieved: July 3, 2011.
  12. ↑ "Beaver Tails c/n 126.:" dhc-2.com. Retrieved: July 3, 2011.
  13. ↑ Aviation Week and Space Technology, volume 54, 1951
  14. ↑ 14.0 14.1 Taylor 1966, p. 19.
  15. ↑ Taylor 1973, p. 457
  16. ↑ Lua error in package.lua at line 80: module 'strict' not found.
  17. ↑ Grandolini Air Enthusiast Thity-seven, p.40.
  18. ↑ 18.0 18.1 "de Havilland U-6A Beaver." National Museum of the US Air Force. Retrieved: 23 August 2015.
  19. ↑ Swanborough and Bowers 1976, p. 482.
  20. ↑ "De Havilland DHC-2 Beaver." "baaa-acro.com. Retrieved: June 3, 2011.
Bibliography
  • Donald, David, ed. The Encyclopedia of World Aircraft. Etobicoke, Ontario: Prospero Books, 1997. ISBN 1-85605-375-X.
  • Harnden, Toby.Bandit Country: The IRA and South Armagh. Philadelphia, PA: Coronet Books, 2000. ISBN 0-340-71737-8.
  • Grandolini, Albert. "L'Aviation Royals Khmere: The first 15 years of Cambodian military aviation". Air Enthusiast, Thirty-seven, September–December 1988. pp. 39–47. ISSN 0143-5450.
  • Hotson, Fred W. The de Havilland Canada Story. Toronto: CANAV Books, 1983. ISBN 0-07-549483-3.
  • Pither, Tony. Airline Fleets 2008. Staplefield, West Sussex, UK: Air-Britain (Historians) Ltd, 2008. ISBN 978-0-85130-390-1.
  • Rossiter, Sean. The Immortal Beaver: The World's Greatest Bush Plane. Vancouver: Douglas & McIntyre, 1999. ISBN 1-55054-724-0.
  • Swanborough, Gordon and Peter M. Bowers. United States Navy Aircraft since 1911. London: Putnam, 1976. ISBN 0-370-10054-9.
  • Taylor, John W. R. Jane's All the World's Aircraft 1966-1967. London:Sampson Low, Marston and Company, 1966.
  • Taylor, John W.R. Jane's All the World's Aircraft 1973-1974. London:Jane's Yearbooks, 1973. ISBN 0-354-00117-5

External links

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